To provide a co-curable composite material assembly, a structure and a vehicle which improve the performance and reduce the weight of a structural composite material by obviating the need to include separate UV/visible light-resistant coatings formerly applied to composite material substrates.SOLUTION: Co-curable and co-cured UV/visible light-resistant composite materials are provided which have UV/visible light protection exclusively imparted to a co-curable composite material substrate assembly by a co-curable UV/visible light-resistant fiberglass layer disposed to cover the co-curable and co-cured composite material substrate.SELECTED DRAWING: None
【課題】複合材料基板に以前に付加されていた別個のUV/可視光耐性コーティングを含む必要性をなくすことによって、性能を改善し、構造的な複合材料の重量を低減させた、共硬化可能な複合材料アセンブリ、構造物、及びビークルを提供する。【解決手段】共硬化可能な及び共硬化された複合材料基板をカバーするように配置された共硬化可能なUV/可視光耐性繊維ガラス層によって、共硬化可能な複合材料基板アセンブリに排他的に付与されるUV/可視光保護を有する、共硬化可能な及び共硬化されたUV/可視光耐性複合材料を提供する。【選択図】なし
CO-CURED UV/VISIBLE LIGHT-RESISTANT COMPOSITE MATERIAL FOR STRUCTURAL AIRCRAFT ASSEMBLY
構造的な航空機アセンブリ用の共硬化されたUV/可視光耐性複合材料
2023-10-17
Patent
Electronic Resource
Japanese
IPC: | B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / C08J Verarbeitung , WORKING-UP |
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